Pre-Hardware Optimization and Implementation Of Fast Optics Closed Control Loop Algorithms
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Pre-Hardware Optimization and Implementation Of Fast Optics Closed Control Loop Algorithms
- Publication date
- 2004
- Usage
- Public Domain
- Topics
- HYDROGEN, INFRARED SPECTROSCOPY, PYROXENES, SILICATES, FELDSPARS, IRON, OXYGEN, MINERALOGY, MARS SURFACE, SNC METEORITES, VELOCITY DISTRIBUTION, FOURIER TRANSFORMATION, MELTS (CRYSTAL GROWTH)
- Collection
- nasa_techdocs
- Contributor
- NASA
- Language
- English
- Rights
- Public Domain
One of the main heritage tools used in scientific and engineering data spectrum analysis is the Fourier Integral Transform and its high performance digital equivalent - the Fast Fourier Transform (FFT). The FFT is particularly useful in two-dimensional (2-D) image processing (FFT2) within optical systems control. However, timing constraints of a fast optics closed control loop would require a supercomputer to run the software implementation of the FFT2 and its inverse, as well as other image processing representative algorithm, such as numerical image folding and fringe feature extraction. A laboratory supercomputer is not always available even for ground operations and is not feasible for a night project. However, the computationally intensive algorithms still warrant alternative implementation using reconfigurable computing technologies (RC) such as Digital Signal Processors (DSP) and Field Programmable Gate Arrays (FPGA), which provide low cost compact super-computing capabilities. We present a new RC hardware implementation and utilization architecture that significantly reduces the computational complexity of a few basic image-processing algorithm, such as FFT2, image folding and phase diversity for the NASA Solar Viewing Interferometer Prototype (SVIP) using a cluster of DSPs and FPGAs. The DSP cluster utilization architecture also assures avoidance of a single point of failure, while using commercially available hardware. This, combined with the control algorithms pre-hardware optimization, or the first time allows construction of image-based 800 Hertz (Hz) optics closed control loops on-board a spacecraft, based on the SVIP ground instrument. That spacecraft is the proposed Earth Atmosphere Solar Occultation Imager (EASI) to study greenhouse gases CO2, C2H, H2O, O3, O2, N2O from Lagrange-2 point in space. This paper provides an advanced insight into a new type of science capabilities for future space exploration missions based on on-board image processing for control and for robotics missions using vision sensors. It presents a top-level description of technologies required for the design and construction of SVIP and EASI and to advance the spatial-spectral imaging and large-scale space interferometry science and engineering.
- Addeddate
- 2011-06-11 07:42:07
- Document-source
- CASI
- Documentid
- 20040171285
- Identifier
- nasa_techdoc_20040171285
- Identifier-ark
- ark:/13960/t7xk96k3x
- Nasa-center
- Goddard Space Flight Center
- Ocr
- ABBYY FineReader 8.0
- Online-source
- http://wayback.archive-it.org/1792/20100215191603/http://hdl.handle.net/2060/20040171285
- Original-nasa-rights
- Unclassified; No Copyright; Unlimited; Publicly available; Final Report
- Ppi
- 300
- Updated-added-to-ntrs
- 2008-06-02
- Year
- 2004
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